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عنوان
Advances in predictive models and methodologies for numerically efficient linear and nonlinear analysis of composites /

پدید آورنده
Marco Petrolo, editor.

موضوع
Composite materials-- Mathematical models.,Structural analysis (Engineering)-- Mathematical models.,Composite materials-- Mathematical models.,Structural analysis (Engineering)-- Mathematical models.

رده
TA418
.
9
.
C6

کتابخانه
Center and Library of Islamic Studies in European Languages

محل استقرار
استان: Qom ـ شهر: Qom

Center and Library of Islamic Studies in European Languages

تماس با کتابخانه : 32910706-025

INTERNATIONAL STANDARD BOOK NUMBER

(Number (ISBN
3030119688
(Number (ISBN
3030119696
(Number (ISBN
303011970X
(Number (ISBN
3030119718
(Number (ISBN
9783030119683
(Number (ISBN
9783030119690
(Number (ISBN
9783030119706
(Number (ISBN
9783030119713
Erroneous ISBN
9783030119683

TITLE AND STATEMENT OF RESPONSIBILITY

Title Proper
Advances in predictive models and methodologies for numerically efficient linear and nonlinear analysis of composites /
General Material Designation
[Book]
First Statement of Responsibility
Marco Petrolo, editor.

.PUBLICATION, DISTRIBUTION, ETC

Place of Publication, Distribution, etc.
Cham, Switzerland :
Name of Publisher, Distributor, etc.
Springer,
Date of Publication, Distribution, etc.
2019.

PHYSICAL DESCRIPTION

Specific Material Designation and Extent of Item
1 online resource (xiii, 193 pages) :
Other Physical Details
illustrations (some color)

SERIES

Series Title
PoliTO Springer series,
ISSN of Series
2509-6796

INTERNAL BIBLIOGRAPHIES/INDEXES NOTE

Text of Note
Includes bibliographical references.

CONTENTS NOTE

Text of Note
Intro; Foreword; Preface; Contents; 1 Introduction; 1.1 Advanced Structural Models; 1.2 Damage and Failure; 1.3 Virtual Characterization and Manufacturing Effects; References; Part I High-Fidelity and Computationally Efficient Models for Multiphysics and Design; 2 Variable Kinematic Shell Formulations Accounting for Multi-field Effects for the Analysis of Multi-layered Structures; 2.1 Introduction; 2.2 Basic Equations of Multi-field Problems; 2.3 Laminated Shell Models Considering Multi-field Effects; 2.4 Variable Kinematic Shell Finite Elements; 2.4.1 Refined Theories of Shell Structures
Text of Note
2.4.2 Various Finite Element Shape Functions2.4.3 Node-Dependent Kinematics; 2.5 Weak-Form Governing Equations; 2.6 Selected Numerical Examples; 2.6.1 Hygro-Mechanical Modeling; 2.6.2 Electro-Mechanical Modeling; References; 3 Bistable Buckled Beam-Like Structures by One-Dimensional Hierarchical Modeling; 3.1 Introduction; 3.2 Geometrically Non-linear Hierarchical Models; 3.2.1 Geometrical and Constitutive Equations; 3.2.2 CUF-Based Displacement Field; 3.2.3 Fundamental Nuclei of the Tangent Stiffness Matrix; 3.3 Numerical Results; 3.4 Concluding Remarks; References
Text of Note
4 Multiscale Nonlinear Analysis of Beam Structures by Means of the Carrera Unified Formulation4.1 Introduction; 4.2 Theoretical Background; 4.2.1 Macroscopic Scale; 4.2.2 Microscopic Scale; 4.2.3 Asymptotic Numerical Method; 4.3 Results; 4.4 Conclusions; References; Part II Failure Analysis, Impact and Health-Monitoring; 5 On the Effectiveness of Higher-Order One-Dimensional Models for Physically Nonlinear Problems; 5.1 Introduction; 5.2 Nonlinear Constitutive Equations; 5.2.1 Plasticity; 5.2.2 Cohesive Modeling; 5.3 Structural Theories and Finite Element Formulation
Text of Note
5.3.1 Nonlinear Governing Equations5.3.2 CUF Cohesive Elements; 5.4 Nonlinear Solution Schemes; 5.5 Numerical Applications; 5.5.1 Multilayered Cantilever Beam Under Bending; 5.5.2 Double Cantilever Test; 5.5.3 Nonlinear Response of Randomly Distributed RVE; 5.6 Conclusion; References; 6 Post-buckling Progressive Failure Analysis of Composite Panels Using a Two-Way Global-Local Coupling Approach Including Intralaminar Failure and Debonding; 6.1 Introduction; 6.2 Theory; 6.2.1 Intralaminar Damage; 6.2.2 Interlaminar Damage
Text of Note
6.3 Application of the Two-Way Coupling Procedure to a One-Stringer Composite Panel6.3.1 Reference Model; 6.3.2 Global Model: Linear Material Model; 6.3.3 Local Model: Skin-Stringer Debonding; 6.3.4 Local-Global Transition; 6.3.5 Results; 6.4 Concluding Remarks; References; 7 Mesoscale Hyperelastic Model of a Single Yarn Under High Velocity Transverse Impact; 7.1 Introduction; 7.2 Theory; 7.2.1 General Notions of Transverse Isotropic Hyperelasticity; 7.2.2 The Notion of Physical Invariants; 7.2.3 The Material Model; 7.2.4 Failure Modelling Using Physical Invariants
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SUMMARY OR ABSTRACT

Text of Note
This book gathers contributions addressing issues related to the analysis of composite structures, whose most relevant common thread is augmented numerical efficiency, which is more accurate for given computational costs than existing methods and methodologies. It first presents structural theories to deal with the anisotropy of composites and to embed multifield and nonlinear effects to extend design capabilities and provide methods of augmenting the fidelity of structural theories and lowering computational costs, including the finite element method. The second part of the book focuses on damage analysis; the multiscale and multicomponent nature of composites leads to extremely complex failure mechanisms, and predictive tools require physics-based models to reduce the need for fitting and tuning based on costly and lengthy experiments, and to lower computational costs; furthermore the correct monitoring of in-service damage is decisive in the context of damage tolerance. The third part then presents recent advances in embedding characterization and manufacturing effects in virtual testing. The book summarizes the outcomes of the FULLCOMP (FULLy integrated analysis, design, manufacturing, and health-monitoring of COMPosite structures) research project.

ACQUISITION INFORMATION NOTE

Source for Acquisition/Subscription Address
Springer Nature
Stock Number
com.springer.onix.9783030119690

OTHER EDITION IN ANOTHER MEDIUM

International Standard Book Number
9783030119683
International Standard Book Number
9783030119706
International Standard Book Number
9783030119713

TOPICAL NAME USED AS SUBJECT

Composite materials-- Mathematical models.
Structural analysis (Engineering)-- Mathematical models.
Composite materials-- Mathematical models.
Structural analysis (Engineering)-- Mathematical models.

(SUBJECT CATEGORY (Provisional

SCI096000
TGMD
TGMD

DEWEY DECIMAL CLASSIFICATION

Number
620
.
1/18
Edition
23

LIBRARY OF CONGRESS CLASSIFICATION

Class number
TA418
.
9
.
C6

PERSONAL NAME - ALTERNATIVE RESPONSIBILITY

Petrolo, Marco

ORIGINATING SOURCE

Date of Transaction
20200823082755.0
Cataloguing Rules (Descriptive Conventions))
pn

ELECTRONIC LOCATION AND ACCESS

Electronic name
 مطالعه متن کتاب 

[Book]

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